Eliptical orbit is fit to the current motion
of the reference point according to the selected mean theory.
Read-only property
| [Visual Basic .NET] |
|---|
Public Property ReferencePoint() As IAgCrdnPointRefTo
|
| [C#] |
|---|
public IAgCrdnPointRefTo ReferencePoint {get;}
|
| [Managed C++] |
|---|
public: __property IAgCrdnPointRefTo^ get_ReferencePoint();
|
| [Unmanaged C++] |
|---|
public: HRESULT get_ReferencePoint(
|
| [Java] |
|---|
public IAgCrdnPointRefTo getReferencePoint();
|